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Numerical investigation of slip flow phenomenon on performance characteristics of gas foil journal bearing

机译:滑动流动现象对燃气箔轴颈轴承性能特性的数值研究

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Gas foil bearings (GFBs) are often employed in turbomachinery, particularly in high-speed turbochargers and turboexpanders. These bearings operate at very high speed and under very low clearance. On account of very low clearance, velocity slip can be observed at the gas–solid-interface. This paper investigates the effect of slip on various performance characteristics of the GFB. A model is put forth to predict the pressure and film thickness of a Gas Foil Journal Bearing (GFJB) used in helium-liquefaction turboexpander operating at 240 krpm. The present model addresses the slip at the gas-foil interface. Modified Reynolds equation, assuming first-order slip, is used along with the structural equation, which illustrates the compliant property of the foil. A numerical model is developed by finite difference approximation and solved by an iterative method. Various performance parameters are assessed for the no-slip and slip flow phenomenon in GFJB. The results are compared and a considerable difference is seen between the two models. The conventional Reynolds equation overestimates the load by approximately 8% at 240 krpm. The load-carrying capacity at different values of Knudsen number is also shown.
机译:燃气箔轴承(GFBs)通常用于涡轮机,特别是在高速涡轮增压器和涡轮增压器中。这些轴承在非常高的速度下运行,低间隙非常低。由于间隙非常低,可以在气体固体界面处观察到速度滑移。本文研究了滑动对GFB各种性能特征的影响。提出了一种模型,以预测氦 - 液化涡轮轴承(GFJB)的压力和薄膜厚度在240 krpm下操作的氦气 - 液化涡轮机。本模型解决了气箔界面处的滑动。假设一阶滑动的改进的雷诺式方程与结构方程一起使用,其示出了箔的柔顺性。通过有限差异近似和通过迭代方法解决的数值模型。在GFJB中评估各种性能参数的无滑动和滑动流动现象。比较结果,两种模型之间看到了相当大的差异。传统的雷诺方程在240 krpm以约8%估计负荷大约8%。还示出了knudsen号不同值的承载能力。

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